EP1324817B1 - Procede permettant de produire une membrane composite a composants multiples - Google Patents

Procede permettant de produire une membrane composite a composants multiples Download PDF

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Publication number
EP1324817B1
EP1324817B1 EP01943923.1A EP01943923A EP1324817B1 EP 1324817 B1 EP1324817 B1 EP 1324817B1 EP 01943923 A EP01943923 A EP 01943923A EP 1324817 B1 EP1324817 B1 EP 1324817B1
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EP
European Patent Office
Prior art keywords
preparation
precursor film
polymer
active layer
support layer
Prior art date
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Expired - Lifetime
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EP01943923.1A
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German (de)
English (en)
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EP1324817A4 (fr
EP1324817A1 (fr
Inventor
Sang-Young Lee
Byeong-In Ahn
Soon-Yong Park
You-Jin Kyung
Heon-Sik Song
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LG Chem Ltd
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LG Chemical Co Ltd
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D71/00—Semi-permeable membranes for separation processes or apparatus characterised by the material; Manufacturing processes specially adapted therefor
    • B01D71/06—Organic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D67/00—Processes specially adapted for manufacturing semi-permeable membranes for separation processes or apparatus
    • B01D67/0081—After-treatment of organic or inorganic membranes
    • B01D67/0083—Thermal after-treatment
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D67/00—Processes specially adapted for manufacturing semi-permeable membranes for separation processes or apparatus
    • B01D67/0002—Organic membrane manufacture
    • B01D67/0009—Organic membrane manufacture by phase separation, sol-gel transition, evaporation or solvent quenching
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D67/00—Processes specially adapted for manufacturing semi-permeable membranes for separation processes or apparatus
    • B01D67/0002—Organic membrane manufacture
    • B01D67/0023—Organic membrane manufacture by inducing porosity into non porous precursor membranes
    • B01D67/0025—Organic membrane manufacture by inducing porosity into non porous precursor membranes by mechanical treatment, e.g. pore-stretching
    • B01D67/0027—Organic membrane manufacture by inducing porosity into non porous precursor membranes by mechanical treatment, e.g. pore-stretching by stretching
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D67/00—Processes specially adapted for manufacturing semi-permeable membranes for separation processes or apparatus
    • B01D67/0081—After-treatment of organic or inorganic membranes
    • B01D67/009—After-treatment of organic or inorganic membranes with wave-energy, particle-radiation or plasma
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D69/00—Semi-permeable membranes for separation processes or apparatus characterised by their form, structure or properties; Manufacturing processes specially adapted therefor
    • B01D69/10—Supported membranes; Membrane supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D69/00—Semi-permeable membranes for separation processes or apparatus characterised by their form, structure or properties; Manufacturing processes specially adapted therefor
    • B01D69/12—Composite membranes; Ultra-thin membranes
    • B01D69/1216—Three or more layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D71/00—Semi-permeable membranes for separation processes or apparatus characterised by the material; Manufacturing processes specially adapted therefor
    • B01D71/06—Organic material
    • B01D71/26—Polyalkenes
    • B01D71/261—Polyethylene
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D71/00—Semi-permeable membranes for separation processes or apparatus characterised by the material; Manufacturing processes specially adapted therefor
    • B01D71/06—Organic material
    • B01D71/26—Polyalkenes
    • B01D71/262—Polypropylene
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D71/00—Semi-permeable membranes for separation processes or apparatus characterised by the material; Manufacturing processes specially adapted therefor
    • B01D71/06—Organic material
    • B01D71/30—Polyalkenyl halides
    • B01D71/32—Polyalkenyl halides containing fluorine atoms
    • B01D71/34—Polyvinylidene fluoride
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C55/00—Shaping by stretching, e.g. drawing through a die; Apparatus therefor
    • B29C55/02—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets
    • B29C55/023—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets using multilayered plates or sheets
    • B29C55/026—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets using multilayered plates or sheets of preformed plates or sheets coated with a solution, a dispersion or a melt of thermoplastic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C55/00—Shaping by stretching, e.g. drawing through a die; Apparatus therefor
    • B29C55/02—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets
    • B29C55/04—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets uniaxial, e.g. oblique
    • B29C55/06—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets uniaxial, e.g. oblique parallel with the direction of feed
    • B29C55/065—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets uniaxial, e.g. oblique parallel with the direction of feed in several stretching steps
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/403—Manufacturing processes of separators, membranes or diaphragms
    • H01M50/406—Moulding; Embossing; Cutting
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409—Separators, membranes or diaphragms characterised by the material
    • H01M50/411—Organic material
    • H01M50/414—Synthetic resins, e.g. thermoplastics or thermosetting resins
    • H01M50/417—Polyolefins
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409—Separators, membranes or diaphragms characterised by the material
    • H01M50/411—Organic material
    • H01M50/414—Synthetic resins, e.g. thermoplastics or thermosetting resins
    • H01M50/42—Acrylic resins
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409—Separators, membranes or diaphragms characterised by the material
    • H01M50/411—Organic material
    • H01M50/414—Synthetic resins, e.g. thermoplastics or thermosetting resins
    • H01M50/423—Polyamide resins
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409—Separators, membranes or diaphragms characterised by the material
    • H01M50/411—Organic material
    • H01M50/414—Synthetic resins, e.g. thermoplastics or thermosetting resins
    • H01M50/426—Fluorocarbon polymers
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409—Separators, membranes or diaphragms characterised by the material
    • H01M50/449—Separators, membranes or diaphragms characterised by the material having a layered structure
    • H01M50/457—Separators, membranes or diaphragms characterised by the material having a layered structure comprising three or more layers
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/489—Separators, membranes, diaphragms or spacing elements inside the cells, characterised by their physical properties, e.g. swelling degree, hydrophilicity or shut down properties
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/489—Separators, membranes, diaphragms or spacing elements inside the cells, characterised by their physical properties, e.g. swelling degree, hydrophilicity or shut down properties
    • H01M50/491—Porosity
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D2323/00—Details relating to membrane preparation
    • B01D2323/34—Use of radiation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D2325/00—Details relating to properties of membranes
    • B01D2325/02—Details relating to pores or porosity of the membranes
    • B01D2325/0283—Pore size
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/05—Accumulators with non-aqueous electrolyte
    • H01M10/052—Li-accumulators
    • H01M10/0525—Rocking-chair batteries, i.e. batteries with lithium insertion or intercalation in both electrodes; Lithium-ion batteries
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/05—Accumulators with non-aqueous electrolyte
    • H01M10/056—Accumulators with non-aqueous electrolyte characterised by the materials used as electrolytes, e.g. mixed inorganic/organic electrolytes
    • H01M10/0564—Accumulators with non-aqueous electrolyte characterised by the materials used as electrolytes, e.g. mixed inorganic/organic electrolytes the electrolyte being constituted of organic materials only
    • H01M10/0565—Polymeric materials, e.g. gel-type or solid-type
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E50/00—Technologies for the production of fuel of non-fossil origin
    • Y02E50/30—Fuel from waste, e.g. synthetic alcohol or diesel
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10—Energy storage using batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249978—Voids specified as micro
    • Y10T428/249979—Specified thickness of void-containing component [absolute or relative] or numerical cell dimension
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
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    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249978—Voids specified as micro
    • Y10T428/24998—Composite has more than two layers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
    • Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
    • Y10T428/264—Up to 3 mils
    • Y10T428/265—1 mil or less
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
    • Y10T428/266—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension of base or substrate

Definitions

  • the present invention relates to a method of preparing a multi-component composite membrane.
  • the multi-component composite membrane comprising a support layer and an active layer having a structure as dense as the conventional active layers, which is capable of having pores formed thereon according to process conditions and with improved permeability due to the pores of a controllable size, the composite membrane having characteristics of an active layer, and with an interfacial adhesion strength between the support layer and the active layer strengthened by ion beams irradiation.
  • membranes are currently in use, such as microfiltration membranes, ultrafiltration membranes, gas separation membranes, pervaporation membranes, and reverse osmosis membranes.
  • the membrane relates to a microfiltration membrane, and in particular to a separator comprising polyolefins such as polyethylene and polypropylene, for a rechargeable lithium ion battery.
  • HCPP high crystalline polypropylene
  • the crystallinity of common polypropylenes is less than 50%, but the crystallinity of HCPP is greater than 50% and it is highly isotactic, so that density, melting point, heat of fusion, and crystallization temperature are high, and characteristics such as rigidity, heat-resistance, impact strength, scratch-resistance, and dimensional stability are excellent.
  • WO 99/25464 describes a process for producing a microporous membrane made with only one polymer.
  • a composite membrane is generally prepared by interfacial polymerization, modification of membranes, and dip coating.
  • Dip coating is widely used in order to prepare the composite membrane, by using a microporous membrane such as a microfiltration membrane or an ultrafiltration membrane as a support layer, coating the microporous membrane with a solution of a material used as an active layer, and drying the coated membrane.
  • the composite membrane prepared by dip coating has a support layer comprising regularly-sized pores, and an active layer having a dense structure with few pores.
  • the composite membrane is limited in application, since the active layer has few pores of a size similar to those of the microfiltration or ultrafiltration membranes, and it is easily delaminated due to a weak interfacial adhesion strength between the support layer and the active layer.
  • the composite membrane may be prepared by coating a polymer on the microporous membrane as disclosed in U.S. Patent Nos. 3,249,109 , 4,388,189 , and 5,102,552 .
  • a hydrophilic monomer such as an acrylic acid
  • polymers such as polyethylene oxide are grafted with corona treatment so that the membrane has a modified surface, and in particular so that it has hydrophilicity as disclosed in U.S. Patent Nos. 4,346,142 , 5,085,775 , and 5,294,346 .
  • the membrane has a modified surface and hydrophilicity, the method of graft polymerization is not applied, since the process is complicated and permeability of the membrane is not satisfactory.
  • a separator having regularly-sized pores for a common battery is coated with a polymer electrolyte solution, and it is used as a separator for a rechargeable lithium ion battery as disclosed in U.S. Patent No. 5,716,421 and European Patent No. 0933824A2 .
  • the separator is prepared by the aforementioned method, the membrane has a dense structure, that is, no pores are formed on the surface of the membrane, and permeability (e.g. air permeability) deteriorates, and the interfacial adhesion strength between the support layer and the active layer is inadequate.
  • EP 0 082 393 describes reinforced microporous membranes suitable for the filtration of aqueous fluids, and a process for producing them by impregnating a porous reinforcing web with a polymeric microporous inner membrane and by laminating to each side of said impregnated web at least one polymeric microporous outer membrane, wherein the pore size of the inner membrane is greater than the pore size of the outer membranes.
  • US 4 919 856 describes a method for producing gas separation membranes comprising a microporous support having provided thereon two non-porous coating layer. This method comprises annealing, drawing and heat-setting steps after the coating of the support.
  • It is an object of the present invention to provide a method for preparing a multi-component composite membrane comprising a support layer and an active layer having a structure as dense as the conventional active layers, which is capable of having pores formed thereon according to process conditions and with improved permeability due to the pores of a controllable size, the composite membrane having characteristics of an active layer, and with an interfacial adhesion strength between the support layer and the active layer strengthened by ion beams irradiation.
  • the present invention provides a preparation method of a multi-component composite membrane comprising the steps defined in claim 1
  • the present invention provides a preparation method for a composite membrane that involves coating a common film having no pores with an active material, instead of as in the conventional method of coating a microporous-film with an active material.
  • the composite membrane is prepared by joint-use of a conventional dry process in which the pores are formed by stretching, and a phase inversion that is used with a solution.
  • an ion beam irradiation step is added in the preparation steps to prepare the membrane, an interface bond between a support layer and an active layer is improved.
  • a separator for batteries comprising the multi-component composite membrane and rechargeable lithium ion batteries, and rechargeable lithium ion polymer batteries, comprising the multi-component composite membrane as a separator are described.
  • the preparation method using a conventional dry process is a method in which pores are formed by rupturing a relatively weak amorphous region through cold stretching after orientating a polymer crystalline region in a certain direction, and the orientation uniformity of the crystalline region is critical for characteristics of the membrane.
  • the method using phase inversion is a method in which pores are formed by phase-separation of a polymer and a solvent from the solution under a controlled temperature, or the use of a non-solvent after preparing a polymer solution.
  • an ion beam irradiation process in which gases such as gaseous argon, hydrogen, oxygen, nitrogen, and carbon dioxide are ionized and irradiated to the surface under an atmosphere of reactive gases to be reacted with the ions and the surface when the ionized gases collide with the surface of the membrane.
  • gases such as gaseous argon, hydrogen, oxygen, nitrogen, and carbon dioxide are ionized and irradiated to the surface under an atmosphere of reactive gases to be reacted with the ions and the surface when the ionized gases collide with the surface of the membrane.
  • a precursor film is prepared in one step of the drying process, it is coated with a polymer solution used for an active layer, it is phase-separated from the polymer solution under suitable conditions, and it is stretched, and thereby the membrane is prepared and pores are formed on the membrane.
  • the ion beam irradiation process is performed before the coating process, so that the membrane surface is modified.
  • the composite membrane comprises materials having pores, which are used for the support layer and the active layer, respectively.
  • the pore size and distribution of the support layer and active layer are different from each other, with the pores of the support layer being formed by a stretching process after orientating a polymer crystalline region in a certain direction during the precursor film preparation.
  • the pores of the active layer are formed by a stretching process after forming a densely structured polymer film through phase-inversion. Micro-cracks and micro-pores of the polymer film can be formed according to the phase-inversion conditions before the film is stretched, so the degree of pore formation is controllable according to said phase-inversion conditions.
  • the support layer of the present invention has the same characteristics as a membrane prepared from the conventional dry process, and the active layer has pores with various sizes according to the process conditions.
  • inter-diffusion among the polymer chains of the support layer and active layer improves through high temperature-stretching and heat-setting, and the surface bond between the support layer and the active layer strengthens. When ion beams are irradiated to the layers, the surface bond may further strengthen.
  • the material used for the support layer of the present invention is not limited to a certain material, and it generally includes one or more materials selected from the group consisting of high density polyethylene, low density polyethylene, linear low density polyethylene, polypropylene, high crystalline polypropylene, polyethylene-propylene copolymer, polyethylene-butylene copolymer, polyethylene-hexene copolymer, polyethylene-octene copolymer, polystyrene-butylene-styrene-copolymer, polystyrene-ethylene-butylene-styrene copolymer, polystyrene, polyphenylene oxide, polysulfone, polycarbonate, polyester, polyamide, polyurethane, polyacrylate, polyvinylidene chloride, polyvinylidene fluoride, polysiloxane, polyolefin, ionomer, polymethylpentene, and hydrogenated oligocyclopentadiene (HOCP), and
  • the high crystalline polypropylene preferably has one or more physical properties selected from the group consisting of a density of 0.905 g/cc or more, a melting point of 164 °C or higher, a crystallization temperature of 125 °C or higher, a crystallinity of 50% or greater, an isotacticity of 96% or greater, and an atactic fraction of 5% or less.
  • the polymer of the polymer solution used for the active layer is selected according to the eventual use of the composite membrane, and it preferably includes at least one material selected from the group consisting of polyethylene, polypropylene, polyvinylidene fluoride, polyvinylidene fluoride-hexafluoropropylene copolymer, polyethylene oxide, polypropylene oxide, polybutylene oxide, polyurethane, polyacrylonitrile, polyacrylate, polyacrylic acid, polyamide, polyacrylamide, polyvinylacetate, polyvinylpyrrolidone, polytetraethylene glycol diacrylate, polysulfone, polyphenylene, oxide, polycarbonate, polyester, polyvinylidene chloride, polysiloxane, and a polyolefin inomer, and a derivative thereof.
  • the solvent of the polymer solution is selected according to the polymer used, and it preferably includes at least one solvent selected from 1-methyl-2-pyrrolidone (NMP), acetone, ethanol, n-propanol, n-butanol, n-hexane, cyclohexanol, acetic acid, ethyl acetate, diethyl ether, dimethyl formamide (DMF), dimethylacetamide (DMAc), dioxane, tetrahydrofuran (THF), dimethyl sulfoxide (DMSO), cyclohexane, benzene, toluene, xylene, and water, and a mixture thereof.
  • NMP 1-methyl-2-pyrrolidone
  • acetone ethanol
  • n-propanol n-butanol
  • n-hexane cyclohexanol
  • acetic acid ethyl acetate
  • the polymer solution is preferably used under the following conditions. During the coating process of the polymer solution, a common film having no pores is dip-coated in the polymer solution, with the concentration of the polymer solution preferably being 0.01 wt% or greater. In addition, it is preferable that the drying of the coated polymer is performed at a relative humidity ranging from 1 to 100% under an atmosphere of a gas selected from gases compnsing nitrogen, oxygen, carbon dioxide, and air preferably at a saturated vapor pressure of less than a saturated vapor pressure of the solvent
  • the thickness of the active layer after coating and drying preferably ranges from 0.1 to 20 ⁇ m.
  • the ion beam irradiation is performed under a vacuum ranging from 10 -1 to 10 -6 torr, by activation of electrons and a gas selected from the group consisting of hydrogen, helium, oxygen, nitrogen, carbon dioxide, air, fluorine, neon, argon, krypton, and N 2 O, and a mixture thereof, the aforementioned gas having an energy ranging from 0.01 to 10 6 keV, and irradiation of the ion beams on the surface of the precursor film.
  • the amount of the ion particle ranges from 10 5 to 10 20 ions/ cm 2 .
  • the reactive gases preferably include helium, hydrogen, oxygen, nitrogen, ammoma, carbon monoxide, carbon dioxide, chlorofluorocarbon, methane, and N 2 O, and a mixture thereof, and the flow rate of the reactive gases preferably ranges from 0.5 to 20 ml/minute.
  • the preparation method of the composite membrane according to the present invention comprises the following steps.
  • the preparation steps of the multi-component composite membrane describe the overall processes for preparing a membrane having optimum physical properties, wherein the membrane can be prepared by adding processes depending on physical properties.
  • the support layer preferably has a thickness in the range from 1 to 50 ⁇ m and the pore size of the support layer is preferably within the range from 0.001 to 10 ⁇ m.
  • the pore size of the active layer is preferably equal to or less than 10 ⁇ m.
  • the air permeability of the composite membrane is preferably equal to or less than 7,000 sec /100 cc.
  • the wet-out rate of the composite membrane is preferably equal to or less than 30 seconds.
  • Example 1 Composite membrane prepared from high crystalline polypropylene and Kynar461 (not according to the invention).
  • a high crystalline polypropylene was used for a support layer and a polyvinylidene fluoride (PVDF) was used for an active layer in order to prepare a precursor film, and the precursor film was stretched through a dry process in order to prepare a composite membrane.
  • PVDF polyvinylidene fluoride
  • High crystalline polypropylene was used for a component of a support layer. It has a melting index of 0.50 g/min, a density of 0.91 g/cc, a melting point of 166.5°C measured with a dynamic scanning calorimeter (DSC), a crystallization temperature of 134.5°C, a crystallinity of 57%, isotacticity of 98% measured by C 13 nuclear magnetic resonance (NMR), and an atactic fraction of about 2% measured after dissolution in xylene, and a precursor film was prepared from the high crystalline polypropylene with use of a single screw extruder equipped with T-die and a take-up device. Extrusion temperature and cooling-roll temperature was 220°C and 80°C respectively, take-up speed was 20 m/min, and a draw down rate (DDR) was 60.
  • DDR draw down rate
  • the prepared precursor film was annealed in a dry oven at 150°C for 1 hour.
  • the coated film was mono-axially low-temperature stretched to 50% of the stretching ratio based on the initial length of the film at room temperature.
  • the low-temperature-stretched film was mono-axially high-temperature stretched to 100% of the stretching ratio based on the initial length of the film, at 140°C.
  • Example 2 A composite membrane prepared from high crystallinity polypropylene and Kynar461 with irradiation of ion beams
  • a composite membrane was prepared by same method of Example 1, except that ion beams were irradiated on a precursor film before coating with the Kynar461 solution.
  • the precursor film prepared in the same manner as in Example 1 was placed in a vacuum chamber while keeping the pressure ranging from 10 -5 to 10 -6 torr, argon cations were irradiated to both sides of the precursor film with an ion gun, and simultaneously oxygen used as an reactive gas was injected into the chamber in an amount of 4 ml/min in order to treat the precursor film surface.
  • Energy of the ion beams was 0.5 keV, and the irradiation amount of ions was 10 16 ions/ cm 2 .
  • a composite membrane was prepared in the same manner as in Example 1.
  • Example 3 A membrane prepared from high density polyethylene/ Kynar461. (not according to the invention).
  • a composite membrane was prepared in the same manner as in Example 1, except that high density polyethylene was used for a support layer instead of high crystalline polypropylene.
  • the high density polyethylene had a melt index of 0.3 g/10. min and a density of 0.964 g/cc.
  • a precursor film was prepared in the same manner as in Example 1.
  • the extrusion temperature and cooling-roll temperature of the take-up device were respectively 200°C and 80°C, the take-up speed of the film was 30 m/min, and the draw-down ratio of the prepared precursor film was 80.
  • the prepared precursor film was annealed in a dry oven at 125°C for 1 hour. Both sides of the annealed precursor film were coated with Kynar461 in the same manner as in Example 1.
  • the coated precursor film was mono-axially stretched at room temperature to 50% of the stretching ratio based on the initial length of the film, and then it was immediately mono-axially high-temperature stretched to 50% of the stretching ratio based on the initial length of the film, at 120°C.
  • the high-temperature stretched film was heat-set at 120°C under tension for 10 minutes, and then a composite membrane was prepared by cooling the heat-set film. Table 1 shows properties of the prepared composite membrane.
  • Comparative Example 1 A composite membrane prepared from Celgard2400 and Kynar461
  • An active layer was coated on a microporous membrane by the conventional method.
  • Celgard2400 (a product by Celanese Co.) prepared from only polypropylene was used for the porous membrane as a support layer, Kynar461 solution was coated on the Celgard2400 having pores, and thereby a composite membrane was prepared.
  • Figs. 1 and 2 show that the composite membrane of Comparative Example 1 has no pores, unlike the composite membrane of the examples according to the present invention that have pores formed on the active layer.
  • Table 1 shows properties of the prepared composite membranes. It is shown that the composite membrane prepared from Celgard2400 and Kynar461 had an air permeability too inferior to measure, and the interfacial adhesion strength and wet-out rate of electrolyte were inferior.
  • Example 1 Example 2
  • Example 3 Comparative Example 1 Thickness ( ⁇ m) 20 20 20 20 20 Pore size ( ⁇ m) Support layer 0.3 x 0.1 0.3 x 0.1 0.4 x 0.1 0.3 x 0.1 Active layer 0.8 x 0.3 0.8 x 0.3 0.6 x 0.3 Unable to be measured Air permeability (sec/ 100 cc) 560 565 620 Unable to be measured Interfacial adhesion strength (g f ) 180 250 240 85 Wet-out rate of an electrolyte (sec) 10 8 9 45
  • the composite membrane prepared by the conventional method has a permeability that is too inferior to be measured, but the composite membranes obtained by the present invention have an improved air permeability ranging from 560 to 620 sec/ 100 cc, because both the active layer and the support layer have a dense structure with pores of a controllable size prepared under suitable preparation conditions.
  • the active layer located on the exterior side of the composite membrane has good properties. That is, the support layer of the present invention has the same properties as the membrane prepared by the conventional dry process, and the active layer has pores with various sizes according to the process condition.
  • the composite membrane prepared by the conventional method has an interfacial adhesion strength of 85 g f
  • the composite membrane obtained by the present invention has an improved interfacial adhesion strength ranging from 180 to 250 g f .
  • the improved interfacial adhesion strength results from high-temperature stretching and heat-setting, that is, the interfacial adhesion strength increases because the mutual bond between polymer chains of the support and active layers strengthens.
  • the interfacial adhesion strength improves further by irradiation of ion beams.
  • the wet-out rate improves appreciably, and it is supposed that the improvement of the wet-out rate is due to changes of morphology and an increase of the interfacial adhesion strength.
  • the multi-component composite membrane is also useful for water treatment, hemodialysis, enzyme purification, patches for drug delivery, gas separation, pervaporation, reverse osmosis, and electrolysis separation.

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Claims (12)

  1. Procédé de préparation d'une membrane composite multi-composants comprenant des couches actives et une couche de support placée entre les couches actives, dans laquelle les couches actives et la couche de support sont chacune dotées de leur porosité respective, lequel procédé comporte les étapes suivantes :
    a) préparer un film précurseur par injection, dans une extrudeuse, d'un polymère utilisé pour la couche de support ;
    b) faire recuire le film précurseur en le chauffant à une température inférieure au point de fusion du polymère ;
    c) irradier par faisceaux d'ions l'une ou l'autre des surfaces, ou les deux, du film précurseur recuit, à l'aide d'un gaz réactif ;
    d) revêtir les deux surfaces du film précurseur irradié d'une solution d'un polymère utilisé pour une couche active ;
    e) faire sécher le film précurseur revêtu pour former, par inversion de phases, un film de polymère de couche active, doté de micropores et de microfissures ;
    f) étirer à basse température le film précurseur séché, à une température qui n'est pas supérieure à la température ambiante ;
    g) étirer à haute température le film précurseur déjà étiré à basse température, à une température inférieure aux points de fusion des polymères de couche de support et de couche active ;
    h) et fixer à chaud le film précurseur étiré à haute température, sous tension et à une température inférieure aux points de fusion des polymères de couche de support et de couche active.
  2. Procédé de préparation conforme à la revendication 1, dans lequel, dans l'étape (d), on revêt de la solution de polymère les deux faces du film précurseur, en opérant par immersion.
  3. Procédé de préparation conforme à la revendication 1, dans lequel la concentration de la solution de polymère de l'étape (d) est égale ou supérieure à 0,01 % en poids.
  4. Procédé de préparation conforme à la revendication 1, dans lequel le séchage de l'étape (e) est effectué sous un taux d'humidité relative valant de 1 à 100 %.
  5. Procédé de préparation conforme à la revendication 1, dans lequel le séchage de l'étape (e) est effectué sous la pression de vapeur saturante.
  6. Procédé de préparation conforme à la revendication 1, dans lequel le séchage de l'étape (e) est effectué dans une atmosphère comprenant un gaz choisi dans l'ensemble constitué par de l'azote, de l'oxygène, du dioxyde de carbone, et de l'air.
  7. Procédé de préparation conforme à la revendication 1, dans lequel les étapes de revêtement (d) et de séchage (e) aboutissent à la formation d'une couche active dont l'épaisseur vaut de 0,1 à 20 µm.
  8. Procédé de préparation conforme à la revendication 1, dans lequel l'irradiation par faisceaux d'ions de l'étape (c) est effectuée sous un vide de 10-1 à 10-6 torr.
  9. Procédé de préparation conforme à la revendication 1, dans lequel l'irradiation par faisceaux d'ions de l'étape (c) est effectuée par activation, à l'aide d'électrons, d'un gaz choisi dans l'ensemble formé par les hydrogène, hélium, oxygène, azote, dioxyde de carbone, air, fluor, néon, argon, krypton, protoxyde d'azote (N2O) et leurs mélanges, de telle sorte que le gaz acquière une énergie valant de 0,01 à 106 keV, puis irradiation de la surface du film précurseur par les faisceaux d'ions.
  10. Procédé de préparation conforme à la revendication 1, dans lequel l'intensité de l'irradiation par faisceaux d'ions vaut de 105 à 1020 ions par centimètre carré.
  11. Procédé de préparation conforme à la revendication 1, dans lequel l'irradiation de l'étape (c) est effectuée dans une atmosphère comprenant un gaz choisi dans l'ensemble constitué par les hélium, hydrogène, azote, ammoniac, monoxyde de carbone, dioxyde de carbone, chlorofluorométhane, méthane, protoxyde d'azote (N2O) et leurs mélanges.
  12. Procédé de préparation conforme à la revendication 11, dans lequel le débit du gaz réactif vaut de 0,5 à 20 mL/min.
EP01943923.1A 2000-06-23 2001-06-22 Procede permettant de produire une membrane composite a composants multiples Expired - Lifetime EP1324817B1 (fr)

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PCT/KR2001/001076 WO2001097957A1 (fr) 2000-06-23 2001-06-22 Membrane composite a composants multiples et procede permettant de la produire

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KR20020001035A (ko) 2002-01-09
KR100409017B1 (ko) 2003-12-06
EP1324817A1 (fr) 2003-07-09
JP4209669B2 (ja) 2009-01-14
JP2003535683A (ja) 2003-12-02
CN100531874C (zh) 2009-08-26
WO2001097957A1 (fr) 2001-12-27
US7087269B2 (en) 2006-08-08
CN1383390A (zh) 2002-12-04
TW572775B (en) 2004-01-21
JP4988656B2 (ja) 2012-08-01
US20040213985A1 (en) 2004-10-28
JP2008302359A (ja) 2008-12-18

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